EP3514128A1 - Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers - Google Patents
Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers Download PDFInfo
- Publication number
- EP3514128A1 EP3514128A1 EP18152228.5A EP18152228A EP3514128A1 EP 3514128 A1 EP3514128 A1 EP 3514128A1 EP 18152228 A EP18152228 A EP 18152228A EP 3514128 A1 EP3514128 A1 EP 3514128A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sic
- dms
- graphite substrate
- graphite
- ppb
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 title claims abstract description 487
- 229910010271 silicon carbide Inorganic materials 0.000 title claims abstract description 464
- 238000000034 method Methods 0.000 title claims abstract description 266
- 230000008569 process Effects 0.000 title claims abstract description 203
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 37
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 385
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 344
- 239000010439 graphite Substances 0.000 claims abstract description 344
- 239000000758 substrate Substances 0.000 claims abstract description 270
- LIKFHECYJZWXFJ-UHFFFAOYSA-N dimethyldichlorosilane Chemical compound C[Si](C)(Cl)Cl LIKFHECYJZWXFJ-UHFFFAOYSA-N 0.000 claims abstract description 214
- 238000005229 chemical vapour deposition Methods 0.000 claims abstract description 142
- 238000000151 deposition Methods 0.000 claims abstract description 82
- 239000000463 material Substances 0.000 claims abstract description 74
- 239000004065 semiconductor Substances 0.000 claims abstract description 11
- 239000011148 porous material Substances 0.000 claims description 115
- 230000015572 biosynthetic process Effects 0.000 claims description 89
- 239000010410 layer Substances 0.000 claims description 89
- 239000011247 coating layer Substances 0.000 claims description 61
- 238000000576 coating method Methods 0.000 claims description 57
- 239000013078 crystal Substances 0.000 claims description 45
- 230000008021 deposition Effects 0.000 claims description 44
- 239000000203 mixture Substances 0.000 claims description 38
- 239000012535 impurity Substances 0.000 claims description 36
- 238000010926 purge Methods 0.000 claims description 31
- 239000002245 particle Substances 0.000 claims description 27
- 238000010438 heat treatment Methods 0.000 claims description 24
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 claims description 17
- 238000001802 infusion Methods 0.000 claims description 17
- 238000001816 cooling Methods 0.000 claims description 11
- 230000000694 effects Effects 0.000 claims description 10
- 239000002344 surface layer Substances 0.000 claims description 8
- 230000003247 decreasing effect Effects 0.000 claims description 4
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 abstract description 10
- 229910000077 silane Inorganic materials 0.000 abstract description 10
- 239000002243 precursor Substances 0.000 description 55
- 239000011248 coating agent Substances 0.000 description 47
- 239000012071 phase Substances 0.000 description 34
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 28
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 27
- 239000010949 copper Substances 0.000 description 27
- 239000011572 manganese Substances 0.000 description 27
- 229910052751 metal Inorganic materials 0.000 description 27
- 239000001301 oxygen Substances 0.000 description 27
- 229910052760 oxygen Inorganic materials 0.000 description 27
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 26
- 239000000460 chlorine Substances 0.000 description 26
- 238000011049 filling Methods 0.000 description 26
- 239000007789 gas Substances 0.000 description 26
- 238000011282 treatment Methods 0.000 description 26
- 239000011701 zinc Substances 0.000 description 26
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 25
- 229910052801 chlorine Inorganic materials 0.000 description 25
- 229910052802 copper Inorganic materials 0.000 description 20
- 229910052748 manganese Inorganic materials 0.000 description 20
- 239000002184 metal Substances 0.000 description 20
- 238000005660 chlorination reaction Methods 0.000 description 19
- 229910052725 zinc Inorganic materials 0.000 description 17
- 238000001994 activation Methods 0.000 description 16
- 230000003698 anagen phase Effects 0.000 description 16
- 229910052710 silicon Inorganic materials 0.000 description 16
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 14
- 239000000047 product Substances 0.000 description 14
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 13
- 229910052786 argon Inorganic materials 0.000 description 13
- 229910052757 nitrogen Inorganic materials 0.000 description 13
- 238000000746 purification Methods 0.000 description 13
- 239000010703 silicon Substances 0.000 description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 9
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 9
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 9
- 229910052799 carbon Inorganic materials 0.000 description 9
- -1 hafnium nitride Chemical class 0.000 description 9
- 229910052782 aluminium Inorganic materials 0.000 description 8
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 7
- 230000004913 activation Effects 0.000 description 7
- 238000000137 annealing Methods 0.000 description 7
- 229910052791 calcium Inorganic materials 0.000 description 7
- 239000011575 calcium Substances 0.000 description 7
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 230000003750 conditioning effect Effects 0.000 description 7
- 239000001257 hydrogen Substances 0.000 description 7
- 229910052739 hydrogen Inorganic materials 0.000 description 7
- 229910052742 iron Inorganic materials 0.000 description 7
- 229910052749 magnesium Inorganic materials 0.000 description 7
- 239000011777 magnesium Substances 0.000 description 7
- 238000012986 modification Methods 0.000 description 7
- 230000004048 modification Effects 0.000 description 7
- 229910052750 molybdenum Inorganic materials 0.000 description 7
- 229910052759 nickel Inorganic materials 0.000 description 7
- 229910052719 titanium Inorganic materials 0.000 description 7
- 239000010936 titanium Substances 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 6
- 239000000843 powder Substances 0.000 description 6
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 5
- KZBUYRJDOAKODT-UHFFFAOYSA-N Chlorine Chemical compound ClCl KZBUYRJDOAKODT-UHFFFAOYSA-N 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 230000005587 bubbling Effects 0.000 description 5
- 229910017052 cobalt Inorganic materials 0.000 description 5
- 239000010941 cobalt Substances 0.000 description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 5
- 230000001747 exhibiting effect Effects 0.000 description 5
- 238000005259 measurement Methods 0.000 description 5
- JLUFWMXJHAVVNN-UHFFFAOYSA-N methyltrichlorosilane Chemical compound C[Si](Cl)(Cl)Cl JLUFWMXJHAVVNN-UHFFFAOYSA-N 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 5
- FDNAPBUWERUEDA-UHFFFAOYSA-N silicon tetrachloride Chemical compound Cl[Si](Cl)(Cl)Cl FDNAPBUWERUEDA-UHFFFAOYSA-N 0.000 description 5
- 238000004140 cleaning Methods 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 239000000428 dust Substances 0.000 description 4
- 150000003961 organosilicon compounds Chemical group 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 238000002360 preparation method Methods 0.000 description 4
- 238000001878 scanning electron micrograph Methods 0.000 description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 3
- 229910002091 carbon monoxide Inorganic materials 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- KTQYJQFGNYHXMB-UHFFFAOYSA-N dichloro(methyl)silicon Chemical compound C[Si](Cl)Cl KTQYJQFGNYHXMB-UHFFFAOYSA-N 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 239000005055 methyl trichlorosilane Substances 0.000 description 3
- 239000005048 methyldichlorosilane Substances 0.000 description 3
- 238000002203 pretreatment Methods 0.000 description 3
- 238000004901 spalling Methods 0.000 description 3
- ZDHXKXAHOVTTAH-UHFFFAOYSA-N trichlorosilane Chemical group Cl[SiH](Cl)Cl ZDHXKXAHOVTTAH-UHFFFAOYSA-N 0.000 description 3
- 239000005052 trichlorosilane Substances 0.000 description 3
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 239000003575 carbonaceous material Substances 0.000 description 2
- DMEXFOUCEOWRGD-UHFFFAOYSA-N chloro-[chloro(dimethyl)silyl]oxy-dimethylsilane Chemical compound C[Si](C)(Cl)O[Si](C)(C)Cl DMEXFOUCEOWRGD-UHFFFAOYSA-N 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 239000010408 film Substances 0.000 description 2
- 238000010574 gas phase reaction Methods 0.000 description 2
- 239000007770 graphite material Substances 0.000 description 2
- 125000005843 halogen group Chemical group 0.000 description 2
- HMMGMWAXVFQUOA-UHFFFAOYSA-N octamethylcyclotetrasiloxane Chemical compound C[Si]1(C)O[Si](C)(C)O[Si](C)(C)O[Si](C)(C)O1 HMMGMWAXVFQUOA-UHFFFAOYSA-N 0.000 description 2
- 150000001282 organosilanes Chemical class 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 229910052708 sodium Inorganic materials 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- GNFTZDOKVXKIBK-UHFFFAOYSA-N 3-(2-methoxyethoxy)benzohydrazide Chemical compound COCCOC1=CC=CC(C(=O)NN)=C1 GNFTZDOKVXKIBK-UHFFFAOYSA-N 0.000 description 1
- VXEGSRKPIUDPQT-UHFFFAOYSA-N 4-[4-(4-methoxyphenyl)piperazin-1-yl]aniline Chemical compound C1=CC(OC)=CC=C1N1CCN(C=2C=CC(N)=CC=2)CC1 VXEGSRKPIUDPQT-UHFFFAOYSA-N 0.000 description 1
- 238000012935 Averaging Methods 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000005046 Chlorosilane Substances 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000005388 borosilicate glass Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000010000 carbonizing Methods 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- YGZSVWMBUCGDCV-UHFFFAOYSA-N chloro(methyl)silane Chemical compound C[SiH2]Cl YGZSVWMBUCGDCV-UHFFFAOYSA-N 0.000 description 1
- YGHUUVGIRWMJGE-UHFFFAOYSA-N chlorodimethylsilane Chemical compound C[SiH](C)Cl YGHUUVGIRWMJGE-UHFFFAOYSA-N 0.000 description 1
- KOPOQZFJUQMUML-UHFFFAOYSA-N chlorosilane Chemical class Cl[SiH3] KOPOQZFJUQMUML-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 239000005049 silicon tetrachloride Substances 0.000 description 1
- 239000002210 silicon-based material Substances 0.000 description 1
- 239000002153 silicon-carbon composite material Substances 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- CZDYPVPMEAXLPK-UHFFFAOYSA-N tetramethylsilane Chemical compound C[Si](C)(C)C CZDYPVPMEAXLPK-UHFFFAOYSA-N 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- PQDJYEQOELDLCP-UHFFFAOYSA-N trimethylsilane Chemical compound C[SiH](C)C PQDJYEQOELDLCP-UHFFFAOYSA-N 0.000 description 1
- 238000001947 vapour-phase growth Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5053—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials non-oxide ceramics
- C04B41/5057—Carbides
- C04B41/5059—Silicon carbide
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
- C04B35/522—Graphite
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
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- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/4505—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application
- C04B41/4529—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application applied from the gas phase
- C04B41/4531—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application applied from the gas phase by C.V.D.
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
- C04B41/526—Multiple coating or impregnation with materials having the same composition but different characteristics
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/87—Ceramics
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0209—Pretreatment of the material to be coated by heating
- C23C16/0218—Pretreatment of the material to be coated by heating in a reactive atmosphere
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/04—Coating on selected surface areas, e.g. using masks
- C23C16/045—Coating cavities or hollow spaces, e.g. interior of tubes; Infiltration of porous substrates
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
- C23C16/32—Carbides
- C23C16/325—Silicon carbide
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
- C23C16/45523—Pulsed gas flow or change of composition over time
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/52—Controlling or regulating the coating process
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00241—Physical properties of the materials not provided for elsewhere in C04B2111/00
- C04B2111/00405—Materials with a gradually increasing or decreasing concentration of ingredients or property from one layer to another
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3817—Carbides
- C04B2235/3826—Silicon carbides
Definitions
- the present invention relates to a new process for manufacturing a silicon carbide (SiC) coated body by depositing SiC in a chemical vapor deposition method using dimethyldichlorosilane (DMS) as the silane source on a graphite substrate.
- DMS dimethyldichlorosilane
- a further aspect of the present invention relates to the new silicon carbide coated body, which can be obtained by the new process of the present invention, and to the use thereof for manufacturing articles for high temperature applications, susceptors and reactors, semiconductor materials, and wafer.
- SiC coated bodies are important products in various technical fields and are particularly useful for high temperature applications such as susceptors and wafer for applied materials and reactors, semiconductor materials, chip manufacturing etc..
- SiC coated bodies SiC coated articles
- superior mechanical properties such as a tight connection (adhesion) of the SiC coating layer to the underlying substrate.
- high etch resistance, impact resistance, fracture toughness and/or crack resistance of the SiC coated body are of particular interest.
- To provide oxidation resistance of the coated body it is further required to apply the SiC coating layer homogeneously and continuously, providing an impervious coating layer on the coated substrate surface.
- the inventors of the present invention surprisingly found, that with the new process as described herein, it is possible to deposit SiC not only as a layer coating the surface of the underlying graphite substrate, but to achieve the formation of SiC tendrils growing into the pores of a porous graphite substrate, which provides SiC coated graphite articles with improved physical and mechanical properties.
- the formation of tendrils extending into the porous graphite provides significantly improved mechanical properties as described below in more detail.
- GB 1,128,757 describes methods for preparing SiC and describes CVD methods using either mixtures of hydrogen and a carbon-containing compound and a silicon-containing compound or mixtures of hydrogen and a compound containing both carbon and silicon, to form silicon carbide crystallized on heated surfaces as a dense, substantially impermeable film of predominantly beta-silicon carbide.
- the method is controlled to form stoichiometric silicon carbide.
- EP 0294047 A1 relates to a process for minimizing carbon content in semiconductor materials by pre-treating carbonaceous surfaces used for the preparation of semiconductor materials and mentions the general possibility of coating graphite samples with SiC using CVD and for example DMS as the CVD precursor. Particular process conditions to achieve the formation of SiC tendrils extending into the coated substrate are not described.
- EP 0121797 A2 describes the preparation of carbon-silicon composite articles comprising the deposition of impermeable, uniform SiC-coating layers onto a starting substrate by CVD.
- Example 6 mentions the use of DMS as CVD precursor for encasing substrate fibers with a film.
- Example 9 mentions the deposition of a SiC coating by CVD using methylchlorosilane in and on a molded granular graphite as the substrate to form an intermediate substrate. Particular process conditions to achieve the formation of SiC tendrils extending into a coated porous graphite substrate are not described.
- US 3,925,577 A describes the deposition of SiC onto a porous composite matrix comprising reinforcing carbon fibers coated with carbon and SiC, which are embedded in a deformable resin and carbon-based matrix by the well-known chemical vapor deposition (CVD) method using e.g. DMS in the presence of methane and hydrogen.
- CVD chemical vapor deposition
- the composite matrix is covered by a SiC coating layer, which may penetrate and impregnate the porous structure of the resin substrate.
- the SiC coating layer applied therein exhibits cracks, which have to be filled and sealed subsequently by applying a further outer coating layer, e.g. an aluminum or hafnium nitride coating and a further outer alumina coating or a borosilicate glass to provide a coated article which fulfills the required heat protection and oxidation resistance sufficiently.
- US 3,925,577 A describes a process for producing a coated isotropic graphite member comprising depositing a layer of silicon on a porous graphite body by a gas phase reaction at a temperature below the melting point of the silicon, followed by heating the graphite member with the applied layer of silicon to a temperature to cause the silicon to melt and penetrate the pores of the graphite and cause the silicon to react in situ with the graphite to form a layer of silicon carbide and further depositing by a gas phase reaction a sealing layer of silicon carbide over the underlying, previously reacted silicon carbide layer.
- the graphite used therein is defined to exhibit a porosity equal to about 18 % to 25 % of the member volume, which inter alia is described to be mandatory to provide silicon carbide coated-isotropic fine grain graphite with the desired strength properties. Departing from the defined graphite characteristics is said to lead to composites exhibiting separated, cracked or spalled coating in high temperature applications.
- the process described therein comprises the mandatory step of surface cleaning the heat treated isotropic graphite member, thereby removing all loose surface particles, prior to subjecting the graphite article to the SiC coating step.
- the CVD method described therein is carried out using silicon tetrachloride as the CVD precursor in the presence of hydrogen and methane. Argon may also be present as an inert gas.
- the use of DMS as the CVD precursor or silane source is not mentioned. Particular process conditions to achieve the improved SiC coated articles of the present invention with the formation of SiC tendrils extending into a coated porous graphite substrate are not described.
- US 3,406,044 A describes a process for preparing resistant heating elements, comprising the application of silicon onto a carbonaceous material by using chemical vapor deposition of trichlorosilane.
- a silicon layer is applied to the substrate, which penetrates into the porous substrate and converts therein to a certain amount into SiC.
- a silicon layer is applied, which comprises SiC to a certain but comparably small amount of about 9 %. It is further described therein, that an applied SiC coating does not penetrate through the pores of the graphite substrate in a considerable amount but forms a rather gas-tight impervious coating on the surface of the graphite.
- DMS as the CVD precursor is not mentioned.
- Particular process conditions to achieve the improved SiC coated articles of the present invention with the formation of SiC tendrils extending into a coated porous graphite substrate are not described.
- US 3,622,369 describes a process for depositing stoichiometric silicon carbide on resistively heated wires, using methyldichlorosilane and hydrogen together with a carbonizing gas such as methane in the CVD method. It is described, that with the use of said specific mixture of methyldichlorosilane as the silane source with hydrogen and methane the formation of silicon carbide filaments occurs. However, it is neither described therein, that such SiC filaments may grow into a porous graphite substrate nor that such filaments may be formed under different CVD reaction conditions such as with other CVC precursor materials like DMS in the presence of hydrogen without adding methane gas. In particular, process conditions to achieve the improved SiC coated articles of the present invention with the formation of SiC tendrils extending into a coated porous graphite substrate are not described.
- GB 1,021,662 describes a method of filling pores of a porous substrate by chemical vapor deposition of organosilicon compounds by treating porous bodies with the aim to reduce the porosity and permeability thereof.
- Porous bodies as described therein mainly relate to silicon carbide bodies but also graphite, alumina and other porous inorganic bodies are mentioned.
- the reduction of the porosity is carried out therein by depositing SiC in the pores of the porous bodies using chemical vapor deposition of organosilicon compounds.
- Preferred organosilicon compounds are used which provide a SiC : C ratio of 1 : 1.
- this organosilicon compound is mentioned as possible CVD precursor only in combination with a silicon-yielding compound such as SiCl 4 .
- a silicon-yielding compound such as SiCl 4 .
- Example 3 only one concrete Example describes the deposition of SiC on a carbon substrate, which is Example 3, wherein SiC is deposited on a piece of electrographite having 18 % porosity by carrying out the CVD in the presence of CH 3 SiCl 3 . According to said Example 3 the porosity can be reduced to 15 %, which indicates that the pore filling can only be achieved to a low degree.
- Particular process conditions to achieve the improved SiC coated articles of the present invention with the formation of SiC tendrils extending into a coated porous graphite substrate are not described.
- One object of the present invention was to provide a new process, which allows to prepare articles comprising a SiC coated graphite substrate, which avoid the disadvantages of the prior art processes.
- a further object of the present invention was to provide a process being able to provide SiC coated articles, wherein the SiC coating forms a tightly connected layer on the underlying graphite substrate.
- a further object of the present invention was to provide a process avoiding the formation of cracks and spallings in the SiC coating
- a further object of the present invention was to provide a process for preparing a SiC coated graphite substrate article in a cost and time efficient manner by reducing the required process steps as far as possible.
- a further object of the present invention was to provide a process for preparing graphite substrate based articles with a SiC coating exhibiting on the one hand sufficient mechanical resistance and strength and on the other hand also a maximum of continuity and homogeneity so that the application of additional coatings or sealing layers, e.g. to seal occurring cracks, is not necessary.
- a further object of the present invention was to provide a new and improved SiC coated graphite substrate body having the desired improved properties as described above.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body with an essentially pure SiC coating.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body with a significantly low content of free Si in the SiC coating.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having an improved averaged coefficient of thermal expansion between the graphite substrate and the SiC coating layer.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having an improved residual compressive load in the SiC layer.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having an improved impact resistance.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having an improved fracture toughness.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having an improved adhesion between the graphite substrate and the SiC coating layer.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body exhibiting an improved relation between the size of the outer (upper) surface of the SiC coating layer to the size of the interfacial layer being formed by the SiC tendrils extending into the porous graphite substrate.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having a multilayer SiC coating.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body having such a multilayer SiC coating, wherein at least two SiC layers of different porosity and/or density are present.
- a further object of the present invention was to provide an improved SiC coated graphite substrate body as described herein, further having such a multilayer SiC coating.
- a further object of the present invention was to provide a new process for preparing such improved SiC coated graphite substrate bodies.
- a further object of the present invention was to provide a new method for depositing stoichiometric SiC on a substrate in a CVD method.
- a further object of the present invention was to provide a new method for depositing stoichiometric SiC on a substrate in a CVD method without adding methane gas.
- a further object of the present invention was to provide an improved graphite substrate, in particular for the use and the applications as described herein.
- a further object of the present invention was to provide such an improved graphite substrate having improved purity.
- a further object of the present invention was to provide such an improved graphite substrate having a modified surface porosity.
- a further object of the present invention was to provide such an improved graphite substrate having a specific chlorine content.
- a further object of the present invention was to provide a new method for preparing such an improved graphite substrate.
- a further object of the present invention was to provide an activated graphite substrate with a modified surface porosity, in particular for the use and the applications as described herein.
- a further object of the present invention was to provide such an activated graphite substrate having an improved purity.
- a further object of the present invention was to provide such an activated graphite substrate having a specific chlorine content.
- a further object of the present invention was to provide a new method for preparing such an activated graphite substrate.
- a further object of the present invention was to provide a new method for depositing SiC on a substrate in a CVD method without using argon as purge gas.
- ranges include the lower and upper threshold values. Accordingly, a definition in the sense of "in the range of X and Y" or “in the range between X and Y" of a parameter A means, that A can be any value of X, Y and any value between X and Y. Definitions in the sense of "up to Y” or “at least X” of a parameter A means, that accordingly A may be any value less than Y and Y, or A may be X and any value greater than X, respectively.
- the term "tendril” or “tendrils” describes deposited SiC material, having a specific length and extending from the surface of a porous substrate into the pores, thereby providing a deep-reaching anchor- or hook-like solid connection between an outer SiC layer extending over the surface of a porous substrate with the porous substrate.
- porosity relates to "open porosity", otherwise the growing of the SiC tendrils into the porous graphite substrate would not be possible.
- Scanning Electron Microscope (SEM) measurement as mentioned in the present invention as a determination method e.g. for determination of porosity degree, pore modification, SiC particle sizes, interfacial layer thickness etc., preferably relates to a SEM system using Phenom ProX (5 kV, 10 kV and 15 kV) at room temperature (appr. 24 °C).
- SEM Scanning Electron Microscope
- a first aspect of the invention relates to the process for manufacturing a silicon carbide (SiC) coated body by depositing SiC in a chemical vapor deposition method using dimethyldichlorosilane (DMS) as the silane source on a graphite substrate.
- SiC silicon carbide
- DMS dimethyldichlorosilane
- One aspect of the process of the present invention relates to the preparation of the graphite member used in said process as the graphite substrate.
- the graphite substrate that will form the basis or core of the SiC coated element can be prepared from any suitable graphite element, e.g. by cutting into the desired size and shape.
- a graphite is used having at least 99 % purity.
- the graphite may then be subjected to further treatments, such as in particular a surface treatment for applying a specific surface structure (machining of the graphite).
- a surface treatment for applying a specific surface structure machining of the graphite.
- the surface structure can have variable design and may be applied according to the customers' needs and wishes.
- the surface structure can be applied using conventional methods known in the art.
- the thus pre-treated graphite member forms the so-called graphite pre-product.
- the graphite substrate having an open porosity it is particularly preferred to use a graphite substrate having a porosity degree of ⁇ 6 % and ⁇ 15 %.
- the graphite used in the process of the present invention has a porosity degree of about 6 % to about 13 %, preferably of about 11 % to about 13 %.
- the porosity degree can be determined using known methods, such as in particular by SEM (scanning electron microscope) measurement as indicated above. Said desired degree can already be present in the graphite used for preparing the graphite pre-product.
- the desired porosity degree can also be adjusted in the process steps of the present invention as described herein.
- a further process step relates to a further pre-treatment of the graphite pre-product.
- the graphite pre-product is subjected to a purification and chlorination procedure. Therefore, the individual elements of the graphite pre-product are stacked into a furnace and purged with nitrogen gas under heating to reach about 2000 °C. Chlorine gas is purged into the furnace to carry out the chlorination of the graphite pre-product.
- argon is often used as the purge gas.
- one aspect of the present invention relates to a process for manufacturing a purified graphite member with a modified surface porosity. Such process comprises the specific process steps
- a purified graphite member having a modified surface porosity.
- Said surface porosity modification becomes apparent compared to the surface porosity of the graphite member according to step a), i.e. a graphite member prior to the treatment according to steps b) to g).
- the modification can be determined e.g. in microphotographs or by SEM (scanning electron microscope) measurement as indicated above.
- the surface porosity is modified, e.g. by enlarging the surface pores and forming a surface pore structure providing a kind of funnels or cones, leading inside the porous graphite member.
- such surface porosity modification comprises enlarging the open pore diameter in the graphite surface compared to the open pore diameter of the graphite member according to step a).
- the average open pore diameter in the graphite surface can be increased for at least 35 %, preferably for at least 40 %, preferably for at least 45 %, preferably for at least 50 %, preferably for at least 55 %, preferably for at least 60 %.
- the average open pore diameter in the graphite surface can be increased for more than 60 %, such as e.g. for 60 to 100 %.
- Such surface porosity modification provides a modified surface structure, which promotes and supports the formation of SiC tendrils growing into and extending into the pores of the graphite member, when used in a CVD method according to the present invention.
- step b) nitrogen is preferably purged until the oxygen content in the furnace is about 3.0 %, preferably about 2.5 %. If the oxygen content in step b) is higher than defined herein before heating the porous graphite member in step c) the graphite burns off and the pore structure is at least partly destroyed. If the oxygen content in step b) is lower than defined herein before heating the porous graphite member in step c), then no sufficient modification of the surface porosity can be achieved.
- the oxygen content can be controlled using an oxygen / carbon monoxide meter Bacharach Model 0024-7341.
- step d) purging with nitrogen and heating is preferably continued until the oxygen content is reduced to ⁇ 0.3 %, preferably ⁇ 0.2 %, preferably ⁇ 0.1 %.
- the graphite member having been purged and optionally heated until the desired low oxygen content has been achieved is directly subjected to the chlorination process by starting to heat the graphite member as defined in step f).
- the chlorine gas is preferably purged with 5 to 20, preferably 7 to 10 slpm slpm (standard liter per minute) chlorine gas.
- the flow meter for controlling the flow of chlorine gas can be a flow meter of Sierra Instruments Digital MFC.
- the chlorination treatment of steps e) to g) is carried out for a time period of about 1 to 4 hours, preferably 1 to 3 hours.
- the chlorination treatment of steps e) to g) is carried out at a temperature of not more than 2600 °C.
- the chlorination treatment is controlled to adjust a chlorine content in the porous graphite member to an amount of at least about 20.00 ppb wt., preferably at least about 40.00 ppb wt., preferably at least about 60.00 ppb wt..
- the chlorine content in the porous graphite member is adjusted to an amount of at least about 30.00 ppb wt., preferably at least about 40.00 ppb wt., preferably at least about 50.00 ppb wt..
- the chlorine content in the porous graphite member is adjusted to an amount in the range of about 20.00 to 250.00 ppb wt., preferably of about 30.00 to 250.00 ppb wt., preferably of about 40.00 to 250.00 ppb wt., preferably of about 50.00 to 250.00 ppb wt..
- the chlorine content in the porous graphite member is adjusted to an amount in the range of about 20.00 to 250.00 ppb wt., preferably of about 20.00 to 200.00 ppb wt., preferably of about 20.00 to 175.00 ppb wt., preferably of about 20.00 to 165.00 ppb wt..
- Such chlorine content adjustment is particularly preferred in the above described process with the process steps e) to g).
- the adjusted and above defined chlorine content is in particular achieved in the deeper regions of the porous graphite member and not only in the surface region.
- the above defined preferred chlorine contents can be achieved inside the porous graphite member, in particular in a depth of ⁇ 50 ⁇ m below the main surface.
- the chlorination content in the depth of the graphite member is preferred to achieve the desired degree of purity and to introduce chlorine into the graphite member.
- Said adjustment can in particular be achieved with the aforesaid preferred chlorination treatment conditions.
- the chlorination treatment is carried out to provide a purified porous graphite member, e.g. a graphite member resulting from the above described process step g), comprising one or more of the following impurity elements in an amount of calcium ⁇ 100.00 ppb wt., magnesium ⁇ 100.00 ppb wt., aluminum ⁇ 100.00 ppb wt., titanium ⁇ 20.00 ppb wt., chromium ⁇ 200.00 ppb wt., manganese ⁇ 20.00 ppb wt., copper ⁇ 100.00 ppb wt., iron ⁇ 20.00 ppb wt., cobalt ⁇ 20.00 ppb wt., nickel ⁇ 20.00 ppb wt., zinc ⁇ 100.00 ppb wt., molybdenum ⁇ 300.00 ppb wt.; preferably comprising one or more of the following impurity elements in an amount of calcium ⁇ 50.00
- the chlorination treatment is carried out to provide a porous member having a purity of ⁇ 98 %, preferably ⁇ 99 %.
- the purification process according to the present invention preferably provides a porous graphite member having a total amount of impurities of ⁇ 10.00 ppm wt., preferably ⁇ 5.00 ppm wt., preferably ⁇ 4.00 ppm wt..
- the above described process of purification or purification and surface modification may further comprise a step of annealing the porous graphite member, thereby maintaining the porous graphite member at a temperature of > 1000 °C for reducing stress in the porous graphite member.
- the resulting purified porous graphite member can be subjected to a surface cleaning, thereby removing dust and loose particles from the surface of the treated graphite member.
- a further process step relates to a further pre-treatment of a graphite pre-product or of the purified and chlorinated graphite member described above.
- the graphite pre-product or the purified, chlorinated graphite member described above is subjected to an activation procedure.
- the inventors of the present invention surprisingly found, that in one further aspect of the present invention the application of very specific process conditions are suitable to prepare an activated graphite member with (further) modified surface porosity.
- a further aspect of the present invention relates to a process for manufacturing an activated graphite substrate with a modified surface porosity.
- Such process comprises the specific process steps
- Such process can be carried out in a process chamber, cladded with graphite.
- the process chamber may comprise holding elements, onto which the graphite elements to be treated can be mounted. It is preferred to keep the point(s) of contact between the graphite elements and the holding elements as small as possible.
- the process chamber may be heated. In principle, such process chambers are known.
- Said process may further comprise a step v) of annealing the activated porous graphite substrate by maintaining the activated porous graphite substrate at a temperature of > 1000 °C for reducing stress in the activated porous graphite substrate following step iv).
- the activated porous graphite substrate may be cleaned from surface dust or loose particles.
- the activated porous graphite substrate obtained by said activation process is directly subjected to a chemical vapor deposition treatment, such as described hereinafter.
- the aforesaid process preferably comprises a further step vi), following step iv) or the optional step v), of directly subjecting the activated porous graphite substrate to a CVD treatment.
- a further aspect of the present invention relates to a process for manufacturing an activated graphite substrate with a modified surface porosity, which comprises the specific process steps
- such activated porous graphite substrate being directly subjected to a CVD process without removing dust or loose particles may comprise a kind of powder layer on the surface, such surface powder layer then mainly comprises carbon powder or carbon dust.
- the porous graphite substrate resulting from step iv) or v) may comprise such a surface powder layer having a thickness of 1 to 15 ⁇ m, preferably of 2 to 10 ⁇ m, preferably of 3 to 7 ⁇ m, preferably of > 1 ⁇ m, preferably of > 2 ⁇ m. Accordingly, the activated porous graphite substrate being directly subjected to CVD treatment in step vi) preferably exhibits a respective surface powder layer.
- step ii) of the activation process described above preferably nitrogen is purged until the oxygen content in the process chamber is about 3.0 %, preferably about 2.5 %.
- step iv) purging with nitrogen and heating is preferably continued until the oxygen content is reduced to ⁇ 0.3 %, preferably ⁇ 0.2 %, preferably ⁇ 0.1 %.
- the oxygen content can be controlled using an oxygen / carbon monoxide meter Bacharach Model 0024-7341.
- an oxygen content in step ii) being higher than defined herein before heating the porous graphite member in step iii) is critical. With a higher oxygen content the graphite may burn off and the pore structure is at least partly destroyed. If the oxygen content in step ii) is lower than defined herein before heating the porous graphite member in step iii), then no sufficient activation of the graphite substrate can be achieved.
- the graphite substrate of step i) exhibits a chlorine content of at least about 20.00 ppb wt., preferably at least about 40.00 ppb wt., preferably at least about 60.00 ppb wt..
- the chlorine content in the porous graphite substrate used in step i) is at least about 30.00 ppb wt., preferably at least about 40.00 ppb wt., preferably at least about 50.00 ppb wt..
- the chlorine content in the porous graphite substrate used in step i) is in the range of about 20.00 to 250.00 ppb wt., preferably of about 30.00 to 250.00 ppb wt., preferably of about 40.00 to 250.00 ppb wt., preferably of about 50.00 to 250.00 ppb wt..
- the chlorine content in the porous graphite substrate used in step i) is in the range of about 20.00 to 250.00 ppb wt., preferably of about 20.00 to 200.00 ppb wt., preferably of about 20.00 to 175.00 ppb wt., preferably of about 20.00 to 165.00 ppb wt..
- said preferred chlorine contents are present inside the porous graphite substrate, in particular in a depth of ⁇ 50 ⁇ m below the main surface.
- the porous graphite substrate of step i) of the activation process preferably has a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably about 6 % to about 13 %, preferably of about 11 % to about 13 %.
- the porous graphite substrate of step i) of the activation process preferably has a density as defined above.
- the porous graphite substrate being treated in the activation treatment descried herein can be further purified to the entrapped chlorine content, as explained above.
- the activated porous graphite substrate resulting from the above described process may comprise one or more of the following impurity elements in an amount of calcium ⁇ 100.00 ppb wt., magnesium ⁇ 100.00 ppb wt., aluminum ⁇ 100.00 ppb wt., titanium ⁇ 20.00 ppb wt., chromium ⁇ 200.00 ppb wt., manganese ⁇ 20.00 ppb wt., copper ⁇ 100.00 ppb wt., iron ⁇ 20.00 ppb wt., cobalt ⁇ 20.00 ppb wt., nickel ⁇ 20.00 ppb wt., zinc ⁇ 100.00 ppb wt., molybdenum ⁇ 300.00 ppb wt..
- the activated porous graphite substrate may have a purity of ⁇ 98 %, preferably ⁇ 99 %.
- the activated porous graphite substrate may further have a total amount of impurities of ⁇ 10.00 ppm wt., preferably ⁇ 5.00 ppm wt., preferably ⁇ 4.00 ppm wt..
- the activated porous graphite substrate is directly subjected to a chemical vapor deposition treatment, such CVD treatment can be carried out in the same process chamber. Then, the introduction of H 2 can already be started, if the temperature in the process chamber is > 1000 °C and the oxygen content in the process chamber is below 1.5 %. For example, the process step 2) of the CVD method described below can already start, if such oxygen content of below 1.5 % is reached in the process chamber.
- treated graphite substrates are particularly suitable to support SiC tendril formation in a CVD method using DMS as described herein.
- SiC Silicon carbide
- a further process step relates to the deposition of SiC on porous graphite substrates.
- Preferred porous graphite substrates are purified and chlorinated graphite members resulting from the purification process described above, as well as activated graphite substrates resulting from the activation process described above.
- a key element of the process of the present invention is the formation of the interfacial layer with the SiC filling of the pores of the porous graphite substrate and the subsequent deposition of SiC to form an outer silicon carbide layer on the porous graphite substrate, which is achieved by chemical vapor deposition of dimethyldichlorosilane.
- the chemical vapor deposition (“CVD”, also known as chemical vapor phase deposition “CVPD”) is a well-known technique used to produce high quality, high-performance, solid materials, such as in particular to produce thin films in the semiconductor industry.
- CVD chemical vapor deposition
- CVPD chemical vapor phase deposition
- a substrate is exposed to one or more volatile precursors, which react and/or decompose on the substrate surface to produce the desired deposit.
- organosilanes can be used as the volatile CVD precursor, including simple organosilanes, which may be substituted by one or more halogen atoms, such as mono-, di-, tri- and tetramethyl silane and chlorosilanes, including e.g. methyldichlorosilane, methyltrichlorosilane, tetrachlorosilane (SiCl 4 ), dimethyldichlorosilane, as well as arylsilanes, which may be substituted by halogen atoms.
- halogen atoms such as mono-, di-, tri- and tetramethyl silane and chlorosilanes, including e.g. methyldichlorosilane, methyltrichlorosilane, tetrachlorosilane (SiCl 4 ), dimethyldichlorosilane, as well as arylsilanes, which may be substituted by halogen
- the most common CVD precursor for depositing silicon carbide are trichlorosilane, tetrachlorosilane and methyltrichlorosilane.
- the inventors of the present invention have found that the advantageous product characteristics as described herein can be achieved with the new process of the present invention by using dimethyldichlorosilane ((CH 3 ) 2 SiCl 2 ; also designated as chlorodimethylsilane, abbreviated as DMS), as the CVD precursor. It turned out that with the specific selection of dimethyldichlorosilane as the CVD precursor instead of e.g.
- the more common tetrachlorosilane, trichlorosilane or methyltrichlorosilane (MTS, trichloromethylsilane) in the new process of the present invention it is possible to achieve the improved characteristics of the SiC coated articles as described herein, such as e.g. the hereinafter described SiC grain and crystal size, the SiC tendril formation and the pore filling degree, the formation of the interfacial layer with the described thickness and thus the improved outer SiC coating layer with the improved mechanical properties, homogeneity and continuity etc.
- one further aspect of the present invention relates to a CVD process with very specific CVD process conditions, being suitable to provide a new and improved SiC coating and thus new and improved SiC coated bodies.
- the inventors of the present invention found, that only the specific CVD conditions of using dimethyldichlorosilane (DMS) as the silane source or CVD precursor in the presence of H 2 as the purge gas for depositing SiC on a graphite substrate having an open porosity leads to the formation of SiC tendrils, which grow into the porous structure of the porous graphite substrate, thus extending into the graphite substrate.
- DMS dimethyldichlorosilane
- improved mechanical properties such as a tight connection (adhesion) of the SiC coating layer to the underlying substrate, high etch resistance, impact resistance, fracture toughness and/or crack resistance of the SiC coating as well as oxidation resistance of the coated body, as well as improved homogeneity of the SiC coating.
- a further aspect of the present invention relates to a process for manufacturing a silicon carbide (SiC) coated body (or article), such process comprising the steps
- step 5) it is particularly preferred to deposit not only SiC tendrils in the pores of the graphite, but also a SiC coating on top of the surface of the graphite substrate with the SiC filled pores. Therefore, step 5) - although not mandatory - is preferably also carried out. Certainly, step 5) can be controlled to achieve a SiC surface layer of the desired thickness, e.g. by varying the deposition time and/or the amount of DMS.
- step 2 a pre-conditioning step is included, wherein the porous graphite substrate is pre-treated and activated by purging the process chamber with N 2 and heating to a temperature > 1000 °C, and then directly carrying out step 2).
- pre-treatment step is very similar to the graphite activation process described above.
- the activation process and the CVD method are preferably combined and carried out in the same process chamber.
- such pre-conditioning step preferably comprises purging the process chamber with nitrogen until the oxygen content in the process chamber is about 5.0 %, followed by heating the process chamber to a temperature of at least about 1000 °C, until the oxygen content is ⁇ 0.5 %, preferably ⁇ 0.3 %, preferably ⁇ 0.2 %, preferably ⁇ 0.1 %.
- the oxygen content can be controlled using an oxygen / carbon monoxide meter Bacharach Model 0024-7341.
- the degree of porosity of the graphite substrate to be coated with SiC by CVD plays an important role to achieve the coated articles with the desired superior mechanical properties, such as a tight connection (adhesion) of the SiC coating layer to the underlying substrate, high etch resistance, impact resistance, fracture toughness and/or crack resistance of the SiC coating as well as oxidation resistance of the coated body.
- a graphite substrate to be coated with SiC in the process of the present invention exhibiting a porosity of ⁇ 6 % and ⁇ 15 % turned out to be particularly suitable to achieve the SiC coated articles with the desired properties.
- the graphite substrate to be coated with SiC in the process of the present invention exhibits a porosity of > 6 % to ⁇ 15 % or a porosity in a range of about 6 % to about 14 %, about 6 % to about 13 %, about 6 % to ⁇ 13 %, or a porosity in a range of > 6 % to about 15 %, about 7 % to about 15 %, about 8 % to 15 %, about 9 % to about 15 %, about 10 % to about 15 %, about 11 % to about 15 %, or a porosity in a range of ⁇ 11 % to about 13 %.
- Such preferred ranges are likewise preferred ranges in the purification and chlorination process and the activation process, both as described above, and likewise in the resulting products as described below.
- the degree of porosity according to the present invention can be determined by known methods, including in particular determination of the porosity via SEM measurement, as indicated above.
- the term "tendril” or “tendrils” as used in the present invention describes deposited SiC material, which is grown to extend from the surface of the porous substrate into the pores and thus extends from the surface of the porous substrate into the deeper regions thereof, e.g. in tendril-like or stretched dimension, thus providing a deep-reaching anchor- or hook-like solid connection of the outer SiC layer extending over the surface of the porous substrate with the porous substrate. To achieve sufficient anchoring the tendrils are allowed to grow into the pores until an average length of at least 50 ⁇ m is achieved.
- step 4) is carried out until tendrils of an average length of at least 75 ⁇ m, preferably at least 100 ⁇ m, preferably 75 to 200 ⁇ m are formed.
- the interfacial layer of the SiC coated articles or bodies of the present invention comprises the porous graphite material of the porous graphite substrate with SiC tendrils extending into the pores.
- step 4) is carried out until an interfacial layer having a thickness of at least 100 ⁇ m is formed.
- Said interfacial layer extends from the surface of the porous graphite substrate more or less vertically downwards into the porous graphite substrate and thus forms the interfacial layer or region.
- Said interfacial layer preferably has a thickness of > 100 ⁇ m, more preferably of at least 200 ⁇ m, more preferably of about 200 to about 500 ⁇ m.
- step 3) of the present invention the heated porous graphite substrate is subjected to chemical vapor deposition for depositing the silicon carbide in and on the porous graphite substrate.
- the mixture of DMS and H 2 according to step 3) is preferably obtained by introducing the H 2 gas into the DMS tank, bubbling the H 2 through the DMS in the tank and passing the mixture of DMS and H 2 into the process chamber by purchasing the mixture from the top of the tank.
- an amount of 25 - 45 slpm of the mixture is introduced into the process chamber.
- H 2 is directed through the DMS tank and joined with the DMS. A further amount of H 2 may be purged directly into the process chamber, where it joins with the mixture of DMS and H 2 .
- the flow meter for controlling the flow of the DMS / H 2 mixture can be a flow meter of Sierra Instruments Digital MFC.
- argon is a common purge gas also in CVD methods, however, the inventors found, that no tendril formation occurs when using argon as purge gas in the CVD process of the present invention (or any other process described herein). Therefore, the process is preferably carried out in the absence of argon.
- a SiC layer is further grown on the porous graphite substrate in a first growth phase by continuing chemical vapor deposition of the mixture of dimethyldichlorosilane and H 2 , thus covering the graphite substrate surface.
- the thickness of such SiC coating can be varied, although a surface layer of up to 50 ⁇ m is preferred.
- the process step 5) is carried out until a SiC surface layer of at least 30 ⁇ m, preferably at least 35 ⁇ m, preferably at least 40 ⁇ m, more preferably at least 45 ⁇ m thickness is deposited on the surface of the graphite substrate.
- the thus coated SiC graphite substrate may be subjected to a further step of annealing the coated porous graphite substrate by maintaining the coated porous graphite substrate at a temperature of > 1000 °C for reducing stress in the SiC coating and in the porous graphite substrate.
- Such an annealing step may also be carried out following the pre-conditioning step described above.
- step 6) Due to the positioning of the graphite substrate elements on holding elements said points of contact are not coated with SiC in the CVD process. Therefore, to achieve a homogenous and continuous SiC coating over the whole surface, the following process steps 7) and 8) may be carried out following step 6):
- the second growth phase according to step 8) is carried out applying the same CVD conditions as in the infusion phase and first growth phase. Therefore, in principle the same applies as defined above for the first growth phase.
- An annealing step as described above can also be carried out prior to step 8) and/or prior to the cooling step 6).
- a similar cooling step is carried out after the second growth phase of step 8).
- the coated bodies are preferably subjected to a quality inspection and optionally a purification, thereby removing loose particles and/or protruding crystals.
- the CVD process according to the present invention is controlled, so that the SiC layer deposited onto the graphite substrate in the first growth phase in step 5) is thicker than the SiC layer deposited onto the graphite substrate in the second growth phase in step 8) under the same conditions, in particular with the same DMS amount, and in the same deposition time.
- This can e.g. be achieved by carrying out the above described pre-conditioning step prior to step 2).
- the pre-conditioning step provides an activated surface of the graphite substrate, which provides crystallization points for the SiC crystals and thus accelerates and facilitates the SiC formation in the pores and on the graphite surface.
- Such pre-conditioning step may comprise the process steps i) to v) as described above. It is assumed, that the surface powder layer formed on the graphite substrate in the process steps i) to v) as described above may act as activated surface of the graphite substrate subjected to the CVD treatment in step 1) above.
- the powder on the graphite surface may provide said crystallization points for the SiC crystals and accelerate and facilitate the SiC formation.
- infusion phase very small SiC grains form in the open pores of the porous graphite substrate, which are allowed to grow to SiC crystals to form so-called “tendrils” within the pores.
- small SiC grains are deposited on the upper surface of the graphite substrate to start buildup of the outer SiC layer in the so-called “growth phase”. The small SiC grains are allowed to grow to SiC crystals to form the out SiC layer.
- SiC grain refers to very small crystalline particles formed and deposited in the chemical vapor deposition in step 4) and 5) and 8) by using dimethyldichlorosilane and which mainly comprise silicon carbide.
- Such SiC grains according to the present invention are crystalline and exhibit an average particle size of ⁇ 2 ⁇ m.
- SiC crystal or “SiC crystals” refers to bigger crystalline SiC particles and which are formed in step 4) and 5) and 8) by allowing the deposited SiC grains to grow.
- Such SiC crystals according to the present invention similarly mainly comprise silicon carbide and exhibit an average particle size of ⁇ 2 ⁇ m.
- the SiC crystals according to the present invention exhibit an average particle size > 2 ⁇ m. It is further preferred that the SiC crystals according to the present invention exhibit an average particle size of not more than 30 ⁇ m. More preferably the SiC crystals according to the present invention exhibit an average particle size in the range of about ⁇ 2 to ⁇ 30 ⁇ m.
- the average particle size according to the present invention can be determined by known methods, such as SEM as indicated above.
- the infusion phase of step 4) is controlled to effect the formation of (crystalline) SiC grains having an average particle size of ⁇ 10 ⁇ m can be observed, such as in particular of ⁇ 7 ⁇ m, more particularly of ⁇ 5 ⁇ m or even ⁇ 4 ⁇ m or ⁇ 3 ⁇ m or even ⁇ 2 ⁇ m, formed in the pores during the infusion phase.
- the infusion phase of step 3) is controlled to effect the formation of SiC crystals having an average particle size of not more than 30 ⁇ m ( ⁇ 2 to ⁇ 30 ⁇ m), preferably of not more than 20 ⁇ m ( ⁇ 2 to ⁇ 20 ⁇ m), preferably of not more than 10 ⁇ m ( ⁇ 2 to ⁇ 10 ⁇ m) formed in the pores during the infusion phase by allowing the SiC grains to grow.
- the first and second growth phase of step 5) and 8) are controlled to effect the formation of (crystalline) SiC grains having an average particle size of ⁇ 10 ⁇ m can be observed, such as in particular of ⁇ 7 ⁇ m, more particularly of ⁇ 5 ⁇ m or even ⁇ 4 ⁇ m or ⁇ 3 ⁇ m or even ⁇ 2 ⁇ m on the surface of the graphite substrate during the growth phase and allowing the SiC grains to grow to form SiC crystals having an average particle size of not more than 30 ⁇ m, preferably having an average particle size of ⁇ 2 to ⁇ 30 ⁇ m, preferably of not more than 20 ⁇ m ( ⁇ 2 to ⁇ 20 ⁇ m), preferably of not more than 10 ⁇ m ( ⁇ 2 to ⁇ 10 ⁇ m) on the graphite substrate during the growth phase to form the outer SiC layer.
- a certain amount of SiC grains may also already be formed on the graphite surface during the infusion phase.
- a comparably high degree of pore filling with the deposited SiC material may be advantageous to achieve the desired superior mechanical properties as described above.
- the infusion phase of step 4) is carried out until at least about 70 % of the walls of the open pores of the graphite substrate are coated with the deposited SiC material.
- this shall not define that 70 % of the open porous substrate or 70 % of the total amount of the pores of the porous substrate shall be filled with the SiC, neither are 70 % of the volume of the pores filled with SiC.
- the pore filling degree in accordance with the present invention relates to the degree of coating of the inner walls of the open pores, of which preferably at least 70% are coated with a deposited SiC coating.
- the infusion phase of step 4) is carried out until at least about 75 %, 80 %, 85 %, 90 % of the inner walls of the open pores are coated with the deposited SiC material.
- SiC can be deposited on a porous graphite substrate and in the open pores thereof, having a pore filling degree according to the above definition (i.e. a degree of SiC coating of the inner walls of the pores) of ⁇ 80 % until a depth of about 10 ⁇ m from below the main surface of the coated graphite.
- SiC can be deposited on a porous graphite substrate and in the open pores thereof, having a pore filling degree according to the above definition (i.e. a degree of SiC coating of the inner walls of the pores) of still ⁇ 60 % in a depth of between about 50 to about 10 ⁇ m from below the main surface of the coated graphite.
- SiC can be deposited on a porous graphite substrate and in the open pores thereof, having a pore filling degree according to the above definition (i.e. a degree of SiC coating of the inner walls of the pores) of about 50 % in a depth of between about 100 to about 50 ⁇ m from below the main surface of the coated graphite.
- SiC can be deposited on a porous graphite substrate and in the open pores thereof, having a pore filling degree according to the above definition (i.e. a degree of SiC coating of the inner walls of the pores) of about 40 % in a depth of between about 200 to about 100 ⁇ m from below the main surface of the coated graphite.
- the pore filling degree according to the above definition is up to 50 %.
- the pore filling degree according to the above definition is up to 40 %.
- the degree of pore filling according to the present invention can be determined by SEM measurement as indicated above.
- a further aspect of the process of the present invention relates to the formation of so called tendrils, which act like an anchor for the SiC coating in the porous substrate.
- the process of the present invention is in particular controlled to deposit in step 5) and 8) a SiC coating layer in the form of a homogeneous and continuous, essentially impervious layer onto the surface of the graphite substrate.
- a SiC coating layer is in particular deposited to be essentially free of cracks, holes, spallings or other noticeable surface defects and exhibits essentially a continuous thickness over the whole coated surface area (despite the lacks of coating in the first growth phase due to the holding members).
- the SiC material deposited in the pores in step 4) and/or on the surface in steps 5) and/or 8) comprises at least 90 wt.% pure silicon carbide (SiC).
- the SiC material deposited in the steps 4), 5) and/or 8) comprises at least 91 wt.% at least 92 wt.%, at least 93 wt.%, at least 94 wt.%, at least 95 wt.%, or at least 96 wt.% silicon carbide (SiC). More preferably, the SiC material deposited in the steps 4), 5) and/or 8) comprises at least 97 wt.% SiC, in each case relative to the total weight of the deposited SiC material.
- the SiC material deposited in the steps 4), 5) and/or 8) of the process of the present invention further comprises not more than about 10 wt.%, not more than about 9 wt.%, not more than about 8 wt.%, not more than about 7 wt.%, not more than about 6 wt.%, not more than about 5 wt.%, or not more than about 4 wt.% free Si. More preferably, the SiC material deposited in the steps 4), 5) and/or 8) comprises not more than about 3 wt.% free Si, in each case relative to the total weight of the deposited SiC material.
- the SiC material deposited in the steps 4), 5) and/or 8) preferably comprises a high purity.
- the aforementioned amounts of (pure) SiC and free Si relate to the SiC material deposited in the pores of the graphite substrate, forming the tendrils and the interfacial layer, and/or depositing on the surface of the graphite substrate in the first and second growth phase, together forming the outer SiC layer. Accordingly, when referring to SiC in the meaning of e.g. "SiC layer”, “SiC coating”, “SiC coated body (article)”, “SiC (pore) filling", "SiC grain(s)” or “SiC crystal(s)” etc.
- the process of the present invention can be applied to any suitable graphite substrate.
- the graphite substrates described herein are used.
- the process of the present invention further comprises a step 6) of cooling the SiC coated body (or article).
- the content of certain metal impurities such as metal elements selected from the group consisting of Na, Mg, Al, Ca, Ti, Cr, Mn, Fe, Co, Ni, Cu, Zn, Mo and W, influences the desired SiC tendril formation.
- the presence of a certain content of metal element impurities selected from Mn, Cu and/or Zn has been found to have a significant impact on the desired SiC tendril formation. More particularly, the presence of a certain content of siloxane impurities together with a certain content of one or more of the metal element impurities selected from Mn, Cu and/or Zn was found to influence the desired SiC tendril formation significantly. Without being bound to theory it is assumed that the presence of certain amounts of such siloxane impurities, as defined below, leads to the formation of a precipitate or gel in the DMS tank, in the evaporator and/or in the vapour-conducting conduit system, which deteriorates the SiC tendril formation.
- such undesired gel formation may occur when certain amounts such siloxane impurities and of one or more of the metal element impurities mentioned above are present, such as in particular when certain amounts of such siloxane impurities and of Mn, Cu and/or Zn are present. Also residual moisture or residual water contents may have a further impact on such undesired gel formation.
- the amounts of such impurities in the DMS precursor material used for the CVD method as defined below have been found as advantageous in view of the desired SiC tendril formation as described herein.
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises a content of siloxane compounds (B) of ⁇ 1.500 wt.%, preferably ⁇ 1.000 wt.%, preferably ⁇ 0.900 wt.%, preferably ⁇ 0.850 wt.%, preferably ⁇ 0.800 wt.%, preferably ⁇ 0.750 wt.%, preferably ⁇ 0.700 wt.%, preferably ⁇ 0.600 wt.%, preferably ⁇ 0.500 wt.%.
- B siloxane compounds
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises a content of siloxane compounds (B) of not more than 0.500 wt.%, preferably not more than 0.450 wt.%, preferably not more than 0.400 wt.%, preferably not more than 0.375 wt.%.
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises ⁇ 1.000 wt.% 1,3-dichloro-1,1,3,3,-tetramethyldisiloxane, preferably ⁇ 0.850 wt.%, preferably ⁇ 0.800 wt.%, preferably ⁇ 0.750 wt.%, preferably ⁇ 0.725 wt.%, preferably ⁇ 0.710 wt.%.
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises ⁇ 0.200 wt.% 1,3-dichloro-1,1,3,5,5,5,-hexamethyltrisiloxane, preferably ⁇ 0.150 wt.%, preferably ⁇ 0.140 wt.%, preferably ⁇ 0.130 wt.%, preferably ⁇ 0.120 wt.%, preferably ⁇ 0.110 wt.%.
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises ⁇ 0.200 wt.% octamethylcyclotetrasiloxane, preferably ⁇ 0.190 wt.%, preferably ⁇ 0.180 wt.%, preferably ⁇ 0.170 wt.%, preferably ⁇ 0.160 wt.%.
- metal element impurities may have an influence on the formation and length of the SiC tendrils, e.g. as explained above.
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- a further aspect of the invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using a dimethyldichlorosilane precursor material, wherein the dimethyldichlorosilane precursor material comprises
- the DMS with the defined purities is particularly used in a chemical vapor deposition method, which is carried out using H 2 as purge gas.
- the dimethyldichlorosilane precursor material is passed into the reaction chamber in a mixture with H 2 .
- the mixture of the dimethyldichlorosilane precursor material and H 2 may be obtained by introducing the H 2 gas into the tank containing the dimethyldichlorosilane precursor material, bubbling the H 2 through the tank and passing the mixture of the dimethyldichlorosilane precursor material and H 2 into the reaction chamber by purchasing the mixture from the top of the tank.
- the dimethyldichlorosilane precursor material is further characterized by a content of one or more of the following elements of calcium ⁇ 60.00 ppb wt., magnesium ⁇ 10.00 ppb wt., aluminium ⁇ 12.00 ppb wt., titanium ⁇ 1.00 ppb wt., chromium ⁇ 60.00 ppb wt., iron ⁇ 25000 ppb wt., cobalt ⁇ 1.00 ppb wt., nickel ⁇ 30.00 ppb wt., zinc ⁇ 40.00 ppb wt., molybdenum ⁇ 10.00 ppb wt..
- a further aspect of the present invention relates to the process as described herein, wherein the dimethyldichlorosilane precursor material is used for depositing silicon carbid on a porous graphite substrate having an open porosity with a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably 6 % to 13 %, more preferably 11 to 13 %.
- the defined DMS purities are similarly suitable and preferred in the CVD process described above.
- the inventors of the present invention further found, that with the specific selection of the CVD conditions as described herein, it is possible to control the CVD method to deposit SiC in essentially stoichiometric amounts.
- a further aspect of the present invention relates to a process for manufacturing a silicon carbide (SiC) coated body in a chemical vapor deposition (CVD) method, using dimethyldichlorosilane as the silicon source and H 2 to form substantially stoichiometric silicon carbide.
- the inventors of the present invention surprisingly found that the deposition of substantially stoichiometric silicon carbide leads to the formation of smaller SiC grains and crystals. With substantially stoichiometric silicon carbide an average SiC grains and crystal size of ⁇ 10 ⁇ m can be observed, such as in particular of ⁇ 7 ⁇ m, more particularly of ⁇ 5 ⁇ m or even ⁇ 4 ⁇ m or ⁇ 3 ⁇ m or ⁇ 2 ⁇ m.
- the size of the deposited SiC grains and crystals increases to about 10 ⁇ m and more. It is however preferred to deposit the SiC with smaller grains and crystal sizes, as smaller grains and crystals form SiC coatings of higher density, whereas larger grains and crystals form SiC coatings of lower density. Therefore the deposition of substantially stoichiometric silicon carbide is desired.
- the amount of free Si in the deposited SiC is preferably controlled to be in the range as defined herein, thereby achieving the desired grains and crystal size as defined above.
- said process is in particular carried out without adding methane gas.
- said process is in particular carried out without using any additional silane source besides dimethyldichlorosilane.
- said process is in particular carried out by passing the dimethyldichlorosilane into the reaction chamber in a gaseous mixture with H 2 .
- said process is in particular carried out by using a mixture of the dimethyldichlorosilane and H 2 , which is obtained by introducing the H 2 gas into the tank containing the dimethyldichlorosilane, bubbling the H 2 through the tank and passing the mixture of the dimethyldichlorosilane and H 2 into the reaction chamber by purchasing the mixture from the top of the tank.
- said process is in particular carried using DMS, which comprises a content of (total) siloxane impurities of ⁇ 2.000 wt.%, preferably ⁇ 1.500 wt.%, preferably ⁇ 1.000 wt.%, preferably ⁇ 0.900 wt.%, preferably ⁇ 0.850 wt.%, preferably ⁇ 0.800 wt.%, preferably ⁇ 0.750 wt.%, preferably ⁇ 0.700 wt.%, preferably ⁇ 0.600 wt.%, preferably ⁇ 0.500 wt.%.
- DMS total siloxane impurities of ⁇ 2.000 wt.%, preferably ⁇ 1.500 wt.%, preferably ⁇ 1.000 wt.%, preferably ⁇ 0.900 wt.%, preferably ⁇ 0.850 wt.%, preferably ⁇ 0.800 wt.%, preferably ⁇ 0.750 wt.%, preferably ⁇ 0.700 wt.%,
- said process is in particular carried using DMS, which comprises a content of
- said process is in particular carried out by depositing SiC from dimethyldichlorosilane as the precursor material on a porous graphite substrate.
- said process is in particular carried out using a porous graphite substrate with an open porosity with a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably 6 % to 13 %, more preferably 11 to 13 %.
- the amount of free Si in the SiC deposited on the graphite substrate comprises not more than about 7 wt.%, preferably not more than about wt. 5 %, more preferably not more than about 3 wt.% free Si.
- the inventors of the present invention further surprisingly found that under the specific CVD conditions as described herein, the particle size of the SiC grains correlate to the amount of DMS introduced into the reaction chamber.
- the introduction of lower amounts of DMS surprisingly leads to the formation of smaller grains and crystals, whereas the introduction of larger amounts of DMS surprisingly leads to the formation of larger grains and crystals.
- Smaller grains and crystals further form SiC coatings of higher density, whereas larger grains and crystals form SiC coatings of lower density.
- the CVD deposition can be controlled to provide multilayer SiC coatings having varying densities.
- a further aspect of the present invention relates to a process for manufacturing a silicon carbide (SiC) coated body comprising at least two SiC layer of different density, the process comprising the steps
- step C further comprises prior to step C) the following step
- said process comprises the following steps G) and H) following step F):
- the amount of DMS is gradually increased.
- the second amount of DMS is twice as much as the first amount in step C).
- a third deposition phase is carried out with a third amount of DMS, which is three times as much as the first amount in step C).
- a third and fourth deposition phase are carried out with a third and fourth amount of DMS, wherein the fourth amount of DMS is four times as much as the first amount in step C).
- the DMS amounts in the deposition phases are controlled to effect the formation of smaller SiC crystals having smaller particle size by introducing a decreased amount of DMS and to effect the formation of larger SiC crystals having a larger particle size by introducing an increased amount of DMS.
- the thickness of the SiC coatings deposited in the deposition phases is varied by carrying out the individual deposition phases for varying time periods.
- the porous graphite substrate of step A) has a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably 6 % to 13 %, more preferably 11 to 13 %.
- the mixture of DMS and H 2 is obtained by introducing the H 2 gas into the DMS tank, bubbling the H 2 through the DMS in the tank and passing the mixture of DMS and H 2 into the process chamber by purchasing the mixture from the top of the tank.
- the dimethyldichlorosilane used for the CVD deposition is characterized by having a content of siloxane impurities as defined above, preferably of ⁇ 2.00 wt.%.
- the dimethyldichlorosilane used for the CVD deposition is characterized by having a content of metal element impurities as defined above, preferably of Mn, Cu and Zn impurities as defined above.
- step B-2 is carried out until tendrils of at least 75 ⁇ m length, preferably at least 100 ⁇ m length, preferably 75 to 200 ⁇ m length are formed.
- the infusion phase of step B-2) is carried out until an interfacial layer is formed, comprising the porous graphite with SiC filled pores and having a thickness of at least 50 ⁇ m, preferably ate least 75 ⁇ m, preferably at least 100 ⁇ m, preferably at least 150 ⁇ m, preferably at least 200 ⁇ m, more preferably about 200 to about 500 ⁇ m, wherein the interfacial layer is located between the graphite substrate and the SiC surface layer formed in steps C) to E) and step H).
- an SiC coated article wherein one or more selected surface areas of the graphite substrate are coated with the outer SiC coating layer. It is also possible to deposit the SiC coating in step E) and/or H) not over a complete surface of the porous graphite substrate but only to selected and discrete areas of a surface of the substrate. This can be achieved e.g. by using a kind of mask as commonly used in established coating techniques.
- a further aspect of the present invention relates to the products being obtainable by the processes of the present invention, comprising the intermediate components such as the graphite substrate as well as the SiC coated articles.
- a further aspect of the present invention relates to the purified graphite member with a modified surface porosity, obtainable by a process as described above.
- such purified graphite member with a modified surface porosity has a chlorine content as defined above, preferably present in the porous graphite member as defined above.
- such purified graphite member with a modified surface porosity has an open porosity with a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably of about 6 % to about 13 %, preferably of about 11 % to about 13 %.
- such purified graphite member with a modified surface porosity has a density as defined above.
- such purified graphite member with a modified surface porosity has a purity as defined above.
- the purified graphite member with a modified surface porosity as described herein may preferably be used as a substrate in a silicon carbide coated graphite article.
- the purified graphite member with a modified surface porosity as defined herein is suitable as a substrate in a chemical vapor deposition (CVD) method for depositing silicon carbide thereon, such as in particular in a CVD method as described herein, using dimethyldichlorosilane (DMS) as the silane source or CVD precursor.
- CVD chemical vapor deposition
- Such purified graphite member with a modified surface porosity as described above are particularly suitable for manufacturing articles for high temperature applications, susceptors and reactors, semiconductor materials, wafer.
- a further aspect of the present invention relates to the activated graphite substrate with a modified surface porosity, obtainable by a process as described above.
- such activated graphite substrate with a modified surface porosity has a chlorine content as defined above, preferably present in the porous graphite substrate as defined above.
- such activated graphite substrate with a modified surface porosity has an open porosity with a porosity degree of ⁇ 6 % and ⁇ 15 %, preferably of about 6 % to about 13 %, preferably of about 11 % to about 13 %.
- such activated graphite substrate with a modified surface porosity has a density as defined above.
- such activated graphite substrate with a modified surface porosity has a purity as defined above.
- the activated graphite substrate with a modified surface porosity as described herein may preferably be used as a substrate in a silicon carbide coated graphite article.
- the activated graphite substrate with a modified surface porosity as defined herein is suitable as a substrate in a chemical vapor deposition (CVD) method for depositing silicon carbide thereon, such as in particular in a CVD method as described herein, using dimethyldichlorosilane (DMS) as the silane source or CVD precursor.
- CVD chemical vapor deposition
- Such activated graphite substrate with a modified surface porosity as described above are particularly suitable for manufacturing articles for high temperature applications, susceptors and reactors, semiconductor materials, wafer.
- a further aspect of the present invention covers the silicon carbide coated bodies (or articles) obtained from the process as described above.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles), comprising
- a further aspect of the present invention relates to the silicon carbide coated bodies (or articles) described above, wherein the pores in the interfacial layer III) are filled with SiC in the form of tendrils of at least 75 ⁇ m length, preferably at least 100 ⁇ m length, preferably 75 to 200 ⁇ m length.
- the definition of the pore filling reference is made to the explanations above.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the interfacial layer III) located between the graphite substrate I) and the SiC coating layer(s) II) exhibits a thickness of at least 100 ⁇ m, preferably of > 100 ⁇ m, more preferably of at least 200 ⁇ m, even more preferably of about 200 to about 500 ⁇ m.
- a further aspect of the present invention relates to the silicon carbide coated bodies (or articles) described above, wherein the porous graphite substrate I) exhibits a porosity of > 6 % to ⁇ 15 % or a porosity in a range of about 6 % to about 14 %, about 6 % to about 13 %, about 6 % to ⁇ 13 %, or a porosity in a range of > 6 % to about 15 %, about 7 % to about 15 %, about 8 % to 15 %, about 9 % to about 15 %, about 10 % to about 15 %, about 11 % to about 15 %, or a porosity in a range of ⁇ 11 % to about 13 %.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) described above, wherein the at least one SiC coating layer II) comprises > 90 wt.silicon carbide (SiC).
- the SiC coating layer(s) comprise at least 91 wt.%, at least 92 wt.%, at least 93 wt.%, at least 94 wt.%, at least 95 wt.%, or at least 96 wt.% silicon carbide. More preferably, the SiC coating layer(s) comprises at least 97 wt.SiC, in each case relative to the total weight of the SiC coating layer(s).
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the at least one SiC coating layer II) further comprises not more than about 10 wt.%, not more than about 9 wt.%, not more than about 8 wt.%, not more than about 7 wt.%, not more than about 6 wt.%, not more than about 5 wt.%, or not more than about 4 wt.% free Si. More preferably, the SiC coating layer(s) comprise not more than about 3 wt.% free Si, in each case relative to the total weight of the SiC coating layer(s).
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the SiC coating layer II) covering the graphite substrate I) is a homogeneous and continuous, essentially impervious SiC layer.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the SiC coating layer(s) II) covering the graphite substrate is essentially free of cracks, holes, spallings or other noticeable surface defects and/or exhibits essentially a continuous thickness over the whole coated surface area.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the interfacial layer III) located between the graphite substrate I) and the SiC coating layer II) is formed by the porous graphite, wherein the pores comprise a filling of SiC, and wherein at least 70 % of the walls of the open pores of the graphite are filled with the SiC.
- the pore filling degree in accordance with the present invention relates to the degree of coating of the inner walls of the open pores, of which preferably at least 70% are coated with a deposited SiC coating.
- the interfacial layer III comprises a pore filling degree of at least about 75 %, 80 %, 85 %, 90 % of the walls of the open pores.
- the degree of pore filling can be determined as mentioned above.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the average particle size of the SiC crystals in the filled pores of the interfacial layer III) and/or of the coating layer(s) II) is not more than 30 ⁇ m, preferably > 2 to ⁇ 30 ⁇ m.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the interfacial layer III) located between the graphite substrate I) and the SiC coating layer II) is formed by the porous graphite, wherein the pores comprise a filling of a SiC material, wherein said SiC material comprises > 90 wt-% silicon carbide (SiC).
- SiC material in the pores of the interfacial layer III) comprises at least 91 wt.%, at least 92 wt.%, at least 93 wt.%, at least 94 wt.%, at least 95 wt.%, or at least 96 wt.% silicon carbide.
- the SiC material in the pores of the interfacial layer III) comprises at least 97 wt.% SiC, in each case relative to the total weight of the SiC material in the pore filling.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, wherein the interfacial layer III) located between the graphite substrate I) and the SiC coating layer II) is formed by the porous carbon, wherein the pores comprise a filling of a SiC material, wherein said SiC material further comprises not more than about 10 wt.%, not more than about 9 wt.%, not more than about 8 wt.%, not more than about 7 wt.%, not more than about 6 wt.%, not more than about 5 wt.%, or not more than about 4 wt.% free Si. More preferably, the SiC material in the pores of the interfacial layer III) comprises not more than about 3 wt.% free Si, in each case relative to the total weight of the SiC material in the pore filling.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, comprising the SiC layer II) and optionally also the interfacial layer III) on one or more selected and discrete surface areas of the graphite substrate.
- the interfacial layer of the silicon carbide coated body of the present invention creates a coefficient of thermal expansion (CTE) averaging between the graphite substrate and the SiC coating layer for the entire body.
- CTE coefficient of thermal expansion
- the CTE mismatch between the substrate and the SiC layer can be reduced by about 20 % in a silicon carbide coated body wherein about 20 % of the porous substrate are filled with SIC.
- a further aspect of the present invention relates to a silicon carbide coated body as described herein having an improved coefficient of thermal expansion between the graphite substrate and the SiC coating layer.
- the CTE according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, having an improved residual compressive load in the SiC layer, preferably higher than 190 MPa, preferably higher than 50 MPa.
- the residual compressive load according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, having an improved impact resistance.
- the impact resistance according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, having an improved fracture toughness.
- the fracture toughness according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, having an improved adhesion between the graphite substrate I) and the SiC coating layer II).
- the adhesion between the graphite substrate I) and the SiC coating layer II) according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles) as described herein, exhibiting an improved relation between the size of the outer (upper) surface of the SiC coating layer to the size of the interfacial layer.
- the relation between the size of the outer (upper) surface of the SiC coating layer to the size of the interfacial layer according to the present invention can be determined by known methods.
- a further aspect of the present invention relates to silicon carbide coated bodies (or articles), comprising
- the at least two SiC coating layer(s) II-A) are characterized by different crystal sizes.
- the graphite substrate has an open porosity of ⁇ 6 % and ⁇ 15 %, preferably 6 % to 13 %, more preferably 11 to 13 %.
- the interfacial layer III-A is present, having pores filled with SiC in the form of tendrils of at least 75 ⁇ m length, preferably at least 100 ⁇ m length, preferably 75 to 150 ⁇ m length.
- a further aspect of the present invention relates to the use of the purified, chlorinated and/or activated graphite members, as well as the various silicon carbide coated bodies (or articles) obtainable by the methods as described herein for manufacturing articles for high temperature applications, susceptors and reactors, semiconductor materials, wafer etc.
- a porous graphite member was purified and subjected to a chlorination treatment as described in the present invention.
- the chlorinated graphite member was used as a porous graphite substrate (1) in a CVD deposition method as described herein.
- SiC tendrils (4) according to the present invention were formed in the pores (6) of the accordingly chlorinated graphite substrate.
- a silicon carbide coated body was prepared with the process of the present invention using H 2 as the purge gas.
- argon was used as purge gas.
- a silicon carbide coated body was prepared with the process of the present invention, therein varying the amounts of DMS for preparing a multilayer SiC coating having varying densities (2-A), (2-B), (2-C) etc..
- Deposition phase DMS amount 1. approximately 0.5 g / minute 2. approximately 1.0 g / minute 3. approximately 1.5 g / minute 4. approximately 2.0 g / minute
- the SiC coatings deposited in the first to fourth deposition phase showed varying crystal sizes, which increased with increasing DMS amounts, leading to SiC coating layers with decreasing density.
- a silicon carbide coated body was prepared with the process of the present invention with DMS of varying siloxane impurities.
- a silicon carbide coated body was prepared with the process of the present invention with DMS of varying manganese impurities.
- DMS with the following amounts of manganese impurities were used: metal element DMS Sample A DMS Sample B DMS Sample C manganese (Mn) 2 ppb wt. 11 ppb wt. 150 ppb wt.
- a silicon carbide coated body was prepared with the process of the present invention with DMS of varying copper impurities.
- DMS with the following amounts of copper impurities were used: metal element DMS Sample A DMS Sample B DMS Sample C copper (Cu) 1 ppb wt. 18 ppb wt. 41 ppb wt.
- a silicon carbide coated body was prepared with the process of the present invention with DMS of varying zinc impurities.
- DMS with the following amounts of zinc impurities were used: metal element DMS Sample A DMS Sample B DMS Sample C zinc (Zn) 1 ppb wt. 19 ppb wt. 42 ppb wt.
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Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP18152228.5A EP3514128A1 (de) | 2018-01-18 | 2018-01-18 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
KR1020247006839A KR20240033147A (ko) | 2017-12-27 | 2018-12-22 | 탄화규소 코팅된 몸체를 제조하기 위한 프로세스 |
US16/957,637 US20210017092A1 (en) | 2017-12-27 | 2018-12-22 | Process for manufacturing a silicon carbide coated body |
JP2020535650A JP7078726B2 (ja) | 2017-12-27 | 2018-12-22 | 炭化ケイ素コーティング体を製造するためのプロセス |
KR1020237027314A KR102643483B1 (ko) | 2017-12-27 | 2018-12-22 | 탄화규소 코팅된 몸체를 제조하기 위한 프로세스 |
PCT/US2018/067421 WO2019133560A1 (en) | 2017-12-27 | 2018-12-22 | Process for manufacturing a silicon carbide coated body |
CN202310314995.8A CN116479402A (zh) | 2017-12-27 | 2018-12-22 | 用于制造涂覆碳化硅的主体的工艺 |
EP18837069.6A EP3732155A1 (de) | 2017-12-27 | 2018-12-22 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
CN201880090408.9A CN111788165B (zh) | 2017-12-27 | 2018-12-22 | 用于制造涂覆碳化硅的主体的工艺 |
KR1020207021807A KR102567519B1 (ko) | 2017-12-27 | 2018-12-22 | 탄화규소 코팅된 몸체를 제조하기 위한 프로세스 |
JP2022082076A JP2022127635A (ja) | 2017-12-27 | 2022-05-19 | 炭化ケイ素コーティング体を製造するためのプロセス |
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EP18152228.5A EP3514128A1 (de) | 2018-01-18 | 2018-01-18 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
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EP18152228.5A Withdrawn EP3514128A1 (de) | 2017-12-27 | 2018-01-18 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
EP18837069.6A Pending EP3732155A1 (de) | 2017-12-27 | 2018-12-22 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
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EP18837069.6A Pending EP3732155A1 (de) | 2017-12-27 | 2018-12-22 | Verfahren zur herstellung eines siliciumcarbidbeschichteten körpers |
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US (1) | US20210017092A1 (de) |
EP (2) | EP3514128A1 (de) |
JP (2) | JP7078726B2 (de) |
KR (3) | KR20240033147A (de) |
CN (2) | CN116479402A (de) |
WO (1) | WO2019133560A1 (de) |
Cited By (2)
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WO2022029251A1 (en) * | 2020-08-06 | 2022-02-10 | Sgl Carbon Se | Refractory carbide multilayer |
US11827999B2 (en) | 2021-01-12 | 2023-11-28 | Applied Materials, Inc. | Methods of forming silicon carbide coated base substrates at multiple temperatures |
Families Citing this family (1)
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CN114525495B (zh) * | 2022-01-05 | 2024-03-15 | 湖南德智新材料有限公司 | 一种表面SiC涂层石墨托盘的制备方法及应用 |
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JP2021508662A (ja) | 2021-03-11 |
KR102643483B1 (ko) | 2024-03-07 |
KR20230122187A (ko) | 2023-08-22 |
KR20200103082A (ko) | 2020-09-01 |
KR102567519B1 (ko) | 2023-08-17 |
KR20240033147A (ko) | 2024-03-12 |
CN116479402A (zh) | 2023-07-25 |
WO2019133560A1 (en) | 2019-07-04 |
US20210017092A1 (en) | 2021-01-21 |
CN111788165A (zh) | 2020-10-16 |
CN111788165B (zh) | 2023-04-14 |
JP2022127635A (ja) | 2022-08-31 |
JP7078726B2 (ja) | 2022-05-31 |
EP3732155A1 (de) | 2020-11-04 |
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